The detailed description particularly refers to the accompanying figures in which:
a is a perspective end view of the first stage cone conical member shown in
b is a side perspective view of the cone shown in
c is a side plan view of the cone shown in
a is a perspective view of the interior side of the first stage head showing the air inlet port and the outlet port to the interstage manifold, the first stage head also showing the face for shimming and setting the clearance between the cone and the rotor and the circular rabbet or boss on the head for o-ring sealing;
b is a plan rear view of the exterior side of the first stage head;
c is a cross sectional view of the first stage head taken along view lines 7-7;
d is a plan view looking at the discharge port of the first stage head;
a is a plan front view of the interior side of the second stage head;
b is a side perspective view of the interior side of the second stage head;
c is a cross sectional view of the second stage head taken along view lines 8-8;
a is an end plan view of the interstage manifold;
b is a cross sectional view of the manifold shown in
A two-stage liquid ring vacuum pump 10 adapted to handle large quantities of material carry over without affecting continuous air-flow is shown. Pump 10 includes a rotor 12 that is positioned eccentric relative to body 14. The body 14 has first chamber housing 16 enclosing chamber 16a. The body further has second chamber housing 18 enclosing chamber 18a. As viewed in
The body 14 is adapted to house rotor 12 that includes an intermediate circular wall 48 which separates first stage 38 from second stage 36. The rotor 12 is coupled to drive shaft 49 and is rotated by shaft 49 when power is applied to input shaft 50. The rotor 12 includes first stage blades 52 and second stage blades 54. The rotor 12 and drive shaft 49 are positioned within body 14 so that space 56 is created within first chamber 16a, and space 58 is created within second chamber 18a.
Also positioned within body 14 are first and second stage cones 60, 62. First stage cone 60 is positioned in first chamber 16a and second stage cone 62 is positioned in second chamber 18a. First stage head 32 is coupled to body 14 at an end 201 of first stage housing 16. Second stage head 33 is coupled to body 14 at an end 206 of second stage housing 18, for example, see
The first stage head or end shield 32 is adapted to be coupled to first chamber housing 16 of body 14. Face 79, of first stage head 32, includes a plurality of apertures 92 that permit first stage head 32 to be secured to first chamber housing 16 of body 14. The first stage face, end or side 79, has a surface 179, which is adapted to accept shims 200. The shims 200 create axial spacing or distance between and end wall 201 of first body 14 and internal face surface 179. The spacing is to set end travel clearance between cones 60, 62 and rotor 12. In conical liquid rings pumps, it is critical to properly set the clearance and travel between rotor 12 and first and second stage cones 60, 62. Failure to properly orient these components can cause premature wear and internal leaking which can reduce vacuum pump efficiency.
The first stage head 32 also includes a circular rabbet or boss 110 on face 79 that is adapted to accept an O-ring 202 to permit sealing between the first stage head 32 and body 14. The O-ring seals between the boss's circumferential side wall 203 and an inner side wall 204 towards an end of body 14. A groove 203a to receive the O-ring 202 is in the sidewall 203. An O-ring can be used since the interstage manifold is detachable from first stage head 32.
The first stage head 32 includes recess 80 that is adapted to accept flange 82 of first stage cone 60 as shown, for example, in
The first stage head also includes a pair of bracket members 90 that permit pump 10 to be secured.
First stage cone 60 includes passage 20 into which inlet port 70 opens. The fist stage cone also includes main discharge port 64 opening into discharge port opening 66. First stage cone 60 further includes auxiliary discharge ports 68. Auxiliary discharge ports 68 include two timed vent holes for low speed stability, which improves water handling capabilities and results in hydraulic noise reduction. Auxiliary discharge ports 68 are positioned so that high vacuum capacity is not effected. The vent holes, also, under hogging conditions, at low vacuum, reduce excessive compression in the rotor buckets or spaces 28 between the blades of rotor 52. Correspondingly, peak power requirements at low vacuum are also reduced. The pump can operate at lower than normal tip speeds with these vent holes in the first stage cone The cone 60 also has 4 linearly aligned skew holes 67 to reduce hydraulic noise.
Second stage head or end shield 33 includes intake port 71a, 71b that includes a first chamber 71 a adapted to accept compressed air from interstage manifold 34 and second chamber 71b which is adapted to accept water from interstage manifold 34. Second stage head 36 also includes outlet port 81. The second stage head is adapted to be coupled to second chamber housing 18 of body 14.
The second stage head 33 includes a circular rabbet or boss 110a on face 79a that is adapted to accept an O-ring 202 to permit sealing between the second stage head 33 and body 14. An O-ring 202 can be used since interstage manifold is detachable from second stage head 33. The o-ring 202 seals in the same manner as in the first stage head, i.e., between boss 110a's side wall 207 and an internal side wall 208 of body 14. The o-ring sits in groove 210.
First and second stage heads 32, 33 include outboard bearing carriers 94, 96 that are adapted to the support drive shaft, as shown, for example, in
Both discharge port 30 and intake port 71a, 71b include mating faces 77, 78 that are adapted to accept an O-ring or gasket to seal ports 30, and 71a, 71b to interstage manifold 34.
Mating faces 77, 78 can include a plurality of apertures 76 that are sized to accommodate variations in end travel settings of first and second stage heads 32, 33. Since interstage manifold 34 is removable, it provides the option of being made in lightweight and corrosion resistant materials for cost effective manufacture.
The modular design of pump 10 permits gaskets to be used between the first stage internal face 79 and body end wall 201. The gaskets serve the dual purpose as shims 200 and gaskets 200 when the pump is used in general applications such as those applications used in the power industry. The modular design also permits the use of O-rings using the same casting, but with some additional machining, for more demanding applications, such as those applications in the chemical industry. In demanding industry applications, the shims 200 are used to set end travel only, and O-rings 202 are used to seal between the first stage head 32, second stage head 33 and body 14.
With a gasket only configuration , ie., no o-rings, the gaskets on the first or second stage head could also serve as shims for setting end travel clearance. Any gaskets/shims used on the second stage head would have to be configured to seal around conduit 205. Although the shims or gaskets used in this configuration would not interfere with the use of O-rings 202, in general, when one uses gaskets for sealing duty they do not want o-rings. Thus O-rings 202 would likely be omitted. Conversely when one uses O-rings for sealing they do not want to use gaskets for sealing duty. Any gaskets used would strictly serve as shims.
With an O-ring configuration, the shown second stage internal face end, or side 79a, having surface 179a, is not adapted to accept shims to allow for setting end travel between cones 60,62 and rotor 12. The operating liquid conduit 205 in the second stage head prevents the effective use of shims. The conduit is bordered by a groove 205a to accept an o-ring 209 .
The o-ring 209 seals the conduit 205 to an end face 206 of body 14. A shim, if used, would interfere with the o-ring's ability to seal conduit 205 to end face 206 . Therefore to allow for the use of shims on the second stage head 33, in an o-ring configuration, one would have to reconfigure the second stage head 33, so that it would be compatible with the use of shims.
For instance, one could remove conduit 205 and use an alternative conduit configuration.
In operation the rotation of rotor 12 draws air or gas into inlet 26 of the first stage head and progresses in the direction shown by arrows 112. The air enters first cone passage 20 through inlet port 70. As rotation progresses, the liquid (not shown) from the liquid ring is forced into rotor buckets 28 compressing the air or gas, and a mixture of gas and liquid is then forced out of cone discharge port 64 through first stage head port 66 in the direction shown by arrows 114. The air and gas mixture is discharged from the first stage head through port 30 and enters interstage manifold 34 and progresses as shown by arrows 116.
As the air/gas mixture travels along manifold 34 the mixture enters an expanded region 42 which is characterized by a downwardly sloping ramp 44 leading to a bottom portion 46. The bottom portion is opposite the upper portion 47. In the expanded portion, the liquid portion of the mixture, falls towards the bottom 46 and the air remains above the liquid in upper portion 47. The separation occurs due to velocity reduction and gravity effects. The air enters second stage 33 through chamber 71a. The liquid enters second stage 33 through chamber 71b. Arrows 118 show the air passing from the manifold to the second stage. Arrows 120 show the water passing from the manifold into the second stage.
While embodiments have been illustrated and described in the drawings and foregoing description, such illustrations and descriptions are considered to be exemplary and not restrictive in character, it being understood that only illustrative embodiments have been shown and described and that all changes and modifications that come within the spirit of the invention are desired to be protected. The applicants have provided description and figures which are intended as illustrations of embodiments of the disclosure, and are not intended to be construed as containing or implying limitation of the disclosure to those embodiments. There are a plurality of advantages of the present disclosure arising from various features set forth in the description. It will be noted that alternative embodiments of the disclosure may not include all of the features described yet still benefit from at least some of the advantages of such features. Those of ordinary skill in the art may readily devise their own implementations of the disclosure and associated methods, without undue experimentation, that incorporate one or more of the features of the disclosure and fall within the spirit and scope of the present disclosure and the appended claims.
The present application claims priority from provisional application 60822147 filed Aug. 11, 2006.
Number | Date | Country | |
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60822147 | Aug 2006 | US |